View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 52717U 22056B 25197.87105447 .00000011 00000-0 -89889-5 0 9997
2 52717 86.0040 228.9944 0043143 231.2923 128.4352 13.29579343153759
Epoch (UTC): | 16 July 2025 20:54:19 |
Eccentricity: | 0.0043143 |
inclination: | 86.0040° |
perigee height: | 1116 km |
apogee height: | 1181 km |
right ascension of ascending node: | 228.9944° |
argument of perigee: | 231.2923° |
revolutions per day: | 13.29579343 |
mean anomaly at epoch: | 128.4352° |
orbit number at epoch: | 15375 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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